GB1288449A - - Google Patents
Info
- Publication number
- GB1288449A GB1288449A GB4676470A GB4676470A GB1288449A GB 1288449 A GB1288449 A GB 1288449A GB 4676470 A GB4676470 A GB 4676470A GB 4676470 A GB4676470 A GB 4676470A GB 1288449 A GB1288449 A GB 1288449A
- Authority
- GB
- United Kingdom
- Prior art keywords
- electrodes
- bell
- platform
- housing
- vibrations
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 239000000463 material Substances 0.000 abstract 2
- 101100188555 Arabidopsis thaliana OCT6 gene Proteins 0.000 abstract 1
- 238000013016 damping Methods 0.000 abstract 1
- 229910052734 helium Inorganic materials 0.000 abstract 1
- 239000001307 helium Substances 0.000 abstract 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 abstract 1
- 238000003754 machining Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
- 230000001360 synchronised effect Effects 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/56—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
- G01C19/567—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using the phase shift of a vibration node or antinode
- G01C19/5691—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using the phase shift of a vibration node or antinode of essentially three-dimensional vibrators, e.g. wine glass-type vibrators
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F38/00—Adaptations of transformers or inductances for specific applications or functions
- H01F38/08—High-leakage transformers or inductances
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Gyroscopes (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
Abstract
1288449 Turn-sensitive devices GENERAL MOTORS CORP 1 Oct 1970 [6 Oct 1969] 46764/70 Heading H4D [Also in Division Gl] A device for detecting rotation about a predetermined axis comprises a high-Q resilient bell-shaped member having a centre region supported along said axis by a platform and having side regions depending over and encircling a post carried by the platform, a forcer for imparting first radial vibrations to the side regions, and a sensor located adjacent one of the nodal regions of the resulting radial vibration pattern for detecting second radial vibrations induced at the node (by Coriolis forces) as a result of rotation of the platform about the axis, at least one of the forcer and sensor being fixed to the post within the confines of the bell-shaped member. In the Fig. 1 embodiment the high-Q member is a bell 10 with a stem 16 adjustably supported on a platform 12 having a raised central post 24. A housing 80 is clamped to platform 12 by a ring 260. The first radial vibrations are maintained electrically by a feedback loop including (a) two diametrically opposed forcer electrodes 48, 56 (acting by electrostatic forces on the bell lip) resin-bonded in bores in platform 12 and disposed adjacent vibration anti-nodes, (b) two diametrically opposed sensor electrodes (responsive to changes of capacitance between the bell lip and each sensor electrode) similarly bonded in bores in housing 80 adjcaent vibration antinodes and (c) an oscillator circuit driving the forcer electrodes with a modulated D.C. voltage and synchronized by the sensor electrode outputs. The vibration amplitude is sensed by a level detector coupled to the sensor electrodes and is kept below a selectable maximum value by controlling the modulated D.C. voltage with a signal derived from the level detector. The second radial vibrations, indicative of rotation, are sensed by two diametrically opposed electrodes disposed in housing 80 adjacent the nodes of the first vibrations and provide a rotation-rate output which may be integrated to indicate rotation angle. A signal derived from the latter electrodes is applied with appropriate amplitude and phase to a further pair of forcer electrodes at the said nodes or other nodes of the first vibrations in order to null the second radial vibrations. Air damping of the bell vibrations is reduced by providing cut-outs 255 and 97 in the side walls of post 24 and housing 80, and by partially evacuating the housing and possibly back-filling it with helium. 0-rings 265 and 269 seal the housing while allowing relative angular adjustment of bell 10, platform 12 and housing 80 for optimum positioning of the various electrodes. Electrostatic shielding between the electrodes is provided by bell 10 and by guard sleeves 96, 256 partially surrounding each electrode. Details are given of a method of constructing the apparatus, comprising resinbonding the electrodes and sleeves in bores in material intended to form the platform 12 or housing 80 so that they are insulated from each other and from the bore walls, then machining off the material plus electrodes plus sleeves to conform to the contours of the bell lip.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US86385769A | 1969-10-06 | 1969-10-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1288449A true GB1288449A (en) | 1972-09-06 |
Family
ID=25341945
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4676470A Expired GB1288449A (en) | 1969-10-06 | 1970-10-01 |
Country Status (7)
Country | Link |
---|---|
US (1) | US3678762A (en) |
JP (1) | JPS5025570B1 (en) |
CA (1) | CA932548A (en) |
FR (1) | FR2064166B1 (en) |
GB (1) | GB1288449A (en) |
NL (1) | NL7014665A (en) |
SE (1) | SE359647B (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4157041A (en) * | 1978-05-22 | 1979-06-05 | General Motors Corporation | Sonic vibrating bell gyro |
US4654663A (en) * | 1981-11-16 | 1987-03-31 | Piezoelectric Technology Investors, Ltd. | Angular rate sensor system |
US4951508A (en) * | 1983-10-31 | 1990-08-28 | General Motors Corporation | Vibratory rotation sensor |
USD369305S (en) | 1995-03-13 | 1996-04-30 | Michael Shih | Bell having gyro |
JP3335122B2 (en) | 1998-05-06 | 2002-10-15 | 松下電器産業株式会社 | Angular velocity sensor |
US7296468B2 (en) * | 2005-10-26 | 2007-11-20 | Litton Systems, Inc. | Digital coriolis gyroscope |
US7251900B2 (en) * | 2005-10-26 | 2007-08-07 | Guy Thomas Varty | Methods and systems utilizing intermediate frequencies to control multiple coriolis gyroscopes |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3307409A (en) * | 1959-02-26 | 1967-03-07 | Jr George C Newton | Method of and apparatus for measuring angular motion |
US3241377A (en) * | 1960-01-13 | 1966-03-22 | Jr George C Newton | Method of and apparatus for detecting angular motion |
US3113463A (en) * | 1960-06-08 | 1963-12-10 | United States Time Corp | Inertial angular velocity sensing instrument |
US3408872A (en) * | 1965-10-14 | 1968-11-05 | Air Force Usa | Circumferential flexure vibrating gyroscope |
-
1969
- 1969-10-06 US US863857A patent/US3678762A/en not_active Expired - Lifetime
-
1970
- 1970-06-25 CA CA086492A patent/CA932548A/en not_active Expired
- 1970-10-01 GB GB4676470A patent/GB1288449A/en not_active Expired
- 1970-10-05 SE SE13461/70A patent/SE359647B/xx unknown
- 1970-10-06 FR FR707036078A patent/FR2064166B1/fr not_active Expired
- 1970-10-06 NL NL7014665A patent/NL7014665A/xx not_active Application Discontinuation
- 1970-10-06 JP JP8717370A patent/JPS5025570B1/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
SE359647B (en) | 1973-09-03 |
CA932548A (en) | 1973-08-28 |
JPS5025570B1 (en) | 1975-08-25 |
FR2064166A1 (en) | 1971-07-16 |
DE2046648A1 (en) | 1971-04-22 |
FR2064166B1 (en) | 1974-03-01 |
NL7014665A (en) | 1971-04-08 |
US3678762A (en) | 1972-07-25 |
DE2046648B2 (en) | 1972-11-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |